Since the exhaust valve opens before the exhaust stroke begins, there should be very little pressure by then. But a clogged catalytic converter or muffler would increase the pressure. Also a turbo charger would increase the pressure.
To exactly calculate it would require comprehensive aerodynamic modeling of the complete exhaust system and engine passage way shapes, sizes, timing and RPM.
Not only would one need to know the drag and size of each part of the exhaust path, the resonant characteristics would need to be modeled as well.
This is a dreadful poor answer. Please replace with a better one. -Jesse
The formation of combustion oscillations can occur during an operation of a gas turbine burner. This is also known under the concepts of "combustion chamber humming", "combustion chamber oscillations", "combustion-induced pressure pulsations", "oscillating combustion processes". The combustion oscillations are due to an interaction between the quantity supplied per unit time of combustion air/fuel mixture flowing in the flow duct of the burner. The mixture is ignited after entry into a combustion chamber and burns in a flame, with the momentary combustion conversion in the flame. Combustion conversion designates the quantity of combustion air/fuel mixture converted per unit time during a combustion process in a flame. Pressure fluctuations in the combustion chamber, which can lead to the formation of a stable pressure oscillation, can occur due to a change in the combustion conversion. In addition to an increased production of noise, the combustion oscillations cause an increased mechanical and thermal load on walls associated with the combustion chamber and on other parts belonging to the combustion system. Sandro Garcia
The main function is to spray atomized fuel into the combustion chamber of an internal combustion engine.
Diesel Engine combustion chamber types : Swirl port combustion chamber type and Preignition port combustion chamber type.
Rockets exert force at the upper part of the combustion chamber. This pushes the rocket forward.
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A combustion chamber is where combustion occurs in a controlled fashion. Because the basic idea of a rocket is burning fuels and directing them in the opposite direction to that of travel, a controlled burning - as happens in the combustion chamber - is exactly what a rocket needs to work.
Florence
Superchargers use a spiral type mechanism to force a larger volume of air into the combustion chamber than a naturally aspirated engine can achieve on its own. Using air that is above atmospheric pressure in the combustion chamber allows the fuel to burn more efficiently
Reasons of efficiency. not the least of which is that the pressure generated in the combustion chamber has to fight less "back pressure" (think of it as pressure resistance) at high altitude because the air-pressure is less.
From the combustion of air and fuel in the combustion chamber.
The compression ratio of an internal-combustion engine, or an IC engine as it is more commonly called, is the ratio of the volume the highest capacity of the combustion chamber to its lowest capacity. In the IC engine, the piston makes a stroke, resulting in the compression of the air in the combustion chamber - the ratio between the volume of the cylinder and combustion chamber when the piston is at the bottom of its stroke, and the volume of the combustion chamber when the piston is at the top of its stroke, is the compression ratio.
The fuel/air mixture passes through the intake valve to get into the combustion chamber. After combustion, the spent gasses travel out of the combustion chamber through the exhaust valve.